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Future fundamental combustion research for aeropropulsion systemsPhysical fluid mechanics, heat transfer, and chemical kinetic processes which occur in the combustion chamber of aeropropulsion systems were investigated. With the component requirements becoming more severe for future engines, the current design methodology needs the new tools to obtain the optimum configuration in a reasonable design and development cycle. Research efforts in the last few years were encouraging but to achieve these benefits research is required into the fundamental aerothermodynamic processes of combustion. It is recommended that research continues in the areas of flame stabilization, combustor aerodynamics, heat transfer, multiphase flow and atomization, turbulent reacting flows, and chemical kinetics. Associated with each of these engineering sciences is the need for research into computational methods to accurately describe and predict these complex physical processes. Research needs in each of these areas are highlighted.
Document ID
19850019558
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mularz, E. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
USAAVSCOM-TR-85-C-11
AD-A158778
AIAA PAPER 85-1398
E-2612
NAS 1.15:87049
NASA-TM-87049
Accession Number
85N27870
Funding Number(s)
PROJECT: RTOP 505-31-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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